Thermophysical characteristics of shear-coaxial LOX–H2 flames at supercritical pressure
Author:
Publisher
Elsevier BV
Subject
Physical and Theoretical Chemistry,Mechanical Engineering,General Chemical Engineering
Reference24 articles.
1. Propellant injection in a liquid oxygen/gaseous hydrogen rocket engine
2. Atomization and Breakup of Cryogenic Propellants Under High-Pressure Subcritical and Supercritical Conditions
3. Injection and Mixing Processes in High-Pressure Liquid Oxygen/Gaseous Hydrogen Rocket Combustors
4. Investigation of Cryogenic Propellant Flames Using Computerized Tomography of Emission Images
5. Experimental Investigation of Shear Coaxial Cryogenic Jet Flames
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